A gas turbine engine includes a support structure for attaching the engine to an aircraft pylon. The support structure includes: an engine-side interface member, a pylon-side interface member interfacing to the engine-side interface member, and a top V-shaped connection formation above the engine core and pair of side V-shaped connection formations on opposite lateral sides of the engine core, each V-shaped connection formation being formed by a pair of connection members meeting at a vertex, the vertex of the top V-shaped connection formation joining to the top of the engine-side interface member, the vertices of the side V-shaped connection formations respectively joining to the bottom ends of the engine-side interface member, and the connection members extending forwardly from their respective vertices to join to front fixation points at the core casing.
Support structure for attaching a gas turbine engine to an aircraft pylon
2024-06-18
Patent
Elektronische Ressource
Englisch
Support structure for attaching gas turbine engine to aircraft pylon
Europäisches Patentamt | 2023
|Support structure for attaching gas turbine engine to aircraft pylon
Europäisches Patentamt | 2023
|Support structure for attaching a gas turbine engine to an aircraft pylon
Europäisches Patentamt | 2022
SUPPORT STRUCTURE FOR ATTACHING A GAS TURBINE ENGINE TO AN AIRCRAFT PYLON
Europäisches Patentamt | 2023
|SUPPORT STRUCTURE FOR ATTACHING A GAS TURBINE ENGINE TO AN AIRCRAFT PYLON
Europäisches Patentamt | 2023
|